Original specs for the Mohawk called for it to be aircraft carrier capable. I saw some films in the late 60s of some of the carrier tests by the Navy at Pax River. At that time the plane had a conventional single rudder tail. On a simulated carrier takeoff the pilot apparently flipped the landing gear switch to the up position and relied on the weight-on-wheels switches to keep the gear down. I assume he was trying to get quicker gear retraction on take off. The he stepped on the brakes, ran the engines up to military power and got ready to launch. Unfortunately while running the power up the plane started to bounce a bit. It bounced just enough to take the weight off the switches and retracted the gear at max power and zero airspeed. Probably not a career enhancing day for the pilot. On a simulated carrier landing the plane hooked the arresting cable. Just before it came to a stop the fuselage ripped apart right at the trailing edge of the wings. The tail and most of the fuselage dropped to the ground, the wings and wheel house rolled on down the runway. Soon after the Navy dropped the project.
You might be mixing up the OV-1 Mohawk and the OV-10 Bronco here. Yes, the Mohawk was originally envisioned as a joint Army-USMC project, with an aircraft capable of deployment from light escort carriers. But the Marine Corps (Navy) dropped out a year before the first prototype took to the air. The Bronco, on the other hand, always had an aircraft carrier capability with the Marines. Footage of carrier tests in 1968 here:
Unless it was a later, short lived Navy test effort?
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